The Daimler-Benz DB 601 was a German aircraft engine that was built during World War II. It was a liquid-cooled inverted V12, that powered the Messerschmitt Bf 109, Messerschmitt Bf 110, and many others. Approximately 19,000 601s were produced before being replaced by the improved Daimler-Benz DB 605 in 1942.
| DB 601 | |
|---|---|
Preserved Daimler-Benz DB 601 | |
| Type | Piston V12 aircraft engine |
| National origin | Germany |
| Manufacturer | Daimler-Benz |
| First run | 1935 |
| Major applications | Messerschmitt Bf 109E-F Messerschmitt Bf 110C-F |
| Number built | 19,000 |
| Developed from | Daimler-Benz DB 600 |
| Developed into | |
| Variants | |




At its core, the DB 601 was an improved DB 600 with direct fuel injection. Fuel injection required power to be taken off the drive shaft, but in return, improved low-RPM performance significantly and provided aerobatic performance in maneuvers where early versions of carbureted engines like the British Rolls-Royce Merlin lost power when the carburetor float bowl ran dry.
The 601's fuel injection provided a significant boost in performance which its competitor, the Junkers Jumo 210, did not match for some time. By the time the fuel-injected Jumo 211 arrived, the 601 had already cemented its place as the engine for high-performance designs like fighters, high-speed bombers, and similar roles. The 211 was relegated to use in bombers and transport aircraft. In this respect, the 601 was the counterpart to the Merlin engine of roughly the same size and power.
The DB 601Aa was licence-built in Japan by Aichi as the Atsuta, by Kawasaki as the Ha40, and in Italy by Alfa Romeo as the R.A.1000 R.C.41-I Monsone.
Development
editBased on the guidelines laid down by the German "Reichverkehrsministerium" (Reich Ministry of Transport),[1] in 1930 Daimler-Benz began development of a new aero engine of the 30ย L (1,800ย cuย in) displacement class: a liquid-cooled inverted-vee 12-cylinder piston engine.[2] This was designated F4, and by 1931 two prototypes were running on the test bench.[2] These were followed by the improved F4B, which became the prototype for the DB 600.[2]
In 1933, Daimler-Benz finally received a contract to develop its new engine and to build six examples of the DB 600.[2] For the year after, the DB 600 was the only German aero engine in the 30-litre class.[2] In total, 2,281 DB 600s were built.[2]
The DB 601A-1 was a development of the DB 600 with mechanical direct fuel injection. Like all DB 601s, it had a 33.9 litre displacement.[2] The first DB 601A-1 prototype, designated as F4E, was test run in 1935, and an order for 150 engines was placed in February 1937.[2]
Serial production began in November 1937, and ended in 1943, after 19,000 examples of all types were produced.[2]
Variants
edit- DB 601 A-1
- Up to 1,100ย PS (809ย kW; 1,085ย hp) at sea level with 2,400 rpm, up to 1,020ย PS (750ย kW; 1,006ย hp) at 2,400 rpm and 4,500ย m (14,800ย ft) altitude, B4 fuel
- DB 601 Aa
- Up to 1,175ย PS (864ย kW; 1,159ย hp) at sea level with 2,500 rpm, up to 1,100ย PS (809ย kW; 1,085ย hp) at 2,400 rpm and 3,700ย m (12,100ย ft) altitude, B4 fuel
- DB 601 B-1
- Same as DB601 A-1 for use in Messerschmitt Bf 110 and/or bomber aircraft (different prop/engine ratio, 1:1.88 instead of 1:1.55)
- DB 601 Ba
- Similar to Aa for use in Messerschmitt Bf 110 and/or bomber aircraft (different prop/engine ratio, 1:1.88 instead of 1:1.55)
- DB 601 M
- For use in the Heinkel He 100D 1,175ย PS (864.2ย kW; 1,158.9ย hp)
- DB 601 N
- Up to 1,175ย PS (864ย kW; 1,159ย hp) at sea level and at 4,900ย m (16,100ย ft) altitude with 2,600 rpm, C3 fuel
- Up to 1,270ย PS (934ย kW; 1,253ย hp) at 2,100ย m (6,900ย ft) altitude with 2,600 rpm
- DB 601 P
- Same as DB 601 N for use in Messerschmitt Bf 110 and/or bomber aircraft (different prop/engine ratio, 1:1.88 instead of 1:1.55)
- DB 601 E
- Up to 1,350ย PS (993ย kW; 1,332ย hp) at sea level with 2,700 rpm, up to 1,320ย PS (970ย kW; 1,300ย hp) with 2.700 rpm at 4,800ย m (15,700ย ft) altitude, B4 fuel
- Up to 1,450ย PS (1,066ย kW; 1,430ย hp) at 2,100ย m (6,900ย ft) altitude with 2,700 rpm
- DB 601 F/G
- Same as DB 601 E for use in Messerschmitt Bf 110, Messerschmitt Me 210 and/or bomber aircraft (different prop/engine ratio,1:1.875 (601F), 1:2.06 (601G) instead of 1:1.685)
- DB 606 A/B
- Project initiated in February 1937, to "twin-up" two DB 601As or Es coupled to work on a single propeller shaft with all-up weight of some 1.5 tonnes;[3] for use in Heinkel He 119 (one DB 606) and Messerschmitt Me 261 (twin DB 606) designs, where they worked well in their prototype airframes; saw first combat use with early Heinkel He 177As - 2,700 PS (1,986 kW) at sea level with a mirror-imaged starboard component engine supercharger. Derided as "welded-together engines" by Reichsmarschall Hermann Gรถring in August 1942, from the problems they caused with engine fires in the He 177A during service from their inadequate installation design.[3]
- Alfa-Romeo R.A.1000 R.C.41-I Monsone
- Licence built by Alfa Romeo in Italy
- Aichi Atsuta
- Licence built by Aichi in Japan
- Kawasaki Ha40
- Licence built by Kawasaki in Japan
Applications
edit- DB 601
- Arado Ar 240
- CANSA FC.20
- Dornier Do 215
- Heinkel He 100
- Heinkel He 111 P
- Henschel Hs 130 A-0
- Kawasaki Ki-60
- Messerschmitt Bf 109
- Messerschmitt Bf 110
- Messerschmitt Me 210
- Savoia-Marchetti SM.88
- DB 606
Licensees
edit- Alfa Romeo R.A.1000 R.C.41
Specifications (DB 601 Aa / Ba)
editData from ,[4] Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehรถr-Industrie 1944[5]
General characteristics
- Type: 12-cylinder liquid-cooled supercharged 60ยฐ inverted Vee aircraft piston engine
- Bore: 150ย mm (5.91ย in)
- Stroke: 160ย mm (6.30ย in)
- Displacement: 33.9ย L (2,068.7ย cuย in)
- Length: 1,722ย mm (67.8ย in)
- Width: 739ย mm (29.1ย in)
- Height: 1,027ย mm (40.4ย in)
- Dry weight: 600ย kg (1,323ย lb) dry, unequipped
Components
- Valvetrain: Two intake and two sodium-cooled exhaust valves per cylinder actuated via a single overhead camshaft per cylinder block.
- Supercharger: Gear-driven single-speed centrifugal type supercharger (later, hydraulic-driven) rated to 4,000ย m (13,000ย ft)[6])
- Fuel system: Direct fuel injection
- Oil system: Dry sump with one pressure pump at 0.3โ0.35ย atm (4.4โ5.1ย psi; 0.30โ0.35ย bar) and two scavenge pumps
- Cooling system: Liquid-cooled
Performance
- Power output:
- 1,175ย PS (1,159ย hp; 864ย kW) at 2,500 rpm for takeoff
- 1,100ย PS (1,085ย hp; 809ย kW) at 2,400 rpm at 4,000ย m (13,100ย ft)
- 1,070ย PS (1,055ย hp; 787ย kW) at 2,400 rpm at 3,700ย m (12,100ย ft)
- 1,000ย PS (986ย hp; 735ย kW) at 2,400 rpm (max. continuous / cruise) at 4,000ย m (13,100ย ft)
- Specific power: 34.65ย PS/L (0.56ย hp/cuย in; 25.49ย kW/L)
- Compression ratio: 6.9:1
- Specific fuel consumption: 0.220ย kg/PSh (0.492ย lb/(hpโ h); 0.299ย kg/kWh) at max continuous
- Oil consumption: 0.005โ0.008ย kg/PSh (0.011โ0.018ย lb/(hpโ h); 0.007โ0.011ย kg/kWh) at max continuous
- Power-to-weight ratio: 1.96ย PS/kg (0.88ย hp/lb; 1.44ย kW/kg)
- Reduction gear Spur
- 601Aa 0.645:1
- 601Ba 0.532:1
See also
editRelated development
Comparable engines
- Allison V-1710
- Continental I-1430
- Hispano-Suiza 12Y
- Isotta-Fraschini Asso XI
- Junkers Jumo 211
- Klimov M-103
- Klimov M-105
- Mikulin AM-35
- Rolls-Royce Merlin
Related lists
References
edit- ^ MTU-Museum Triebwerksgeschichte โ gestern, heute und morgen Archived 2016-03-04 at the Wayback Machine, on www.mtu.de (German, PDF, 4,4 MB)
- ^ a b c d e f g h i Mankau&Petrick, 2001. pp. 347-355
- ^ a b Griehl, Manfred; Dressel, Joachim (1998). Heinkel He 177 โ 277 โ 274. Shrewsbury, UK: Airlife Publishing. p.ย 224. ISBNย 1-85310-364-0.
- ^ Tsygulev (1939). Aviacionnye motory voennykh vozdushnykh sil inostrannykh gosudarstv (ะะฒะธะฐัะธะพะฝะฝัะต ะผะพัะพัั ะฒะพะตะฝะฝัั ะฒะพะทะดััะฝัั ัะธะป ะธะฝะพัััะฐะฝะฝัั ะณะพััะดะฐัััะฒ) (in Russian). Moscow: Gosudarstvennoe voennoe izdatelstvo Narkomata Oborony Soyuza SSR. Archived from the original on 2009-03-24.
- ^ Schneider, Helmut (Dipl.Ing.) (1944). Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehรถr-Industrie 1944 (in German) (Facsimile reprint 1986ย ed.). Leipzig: Herm. Beyer Verlag. p.ย 388. ISBNย 381120484X.
{{cite book}}: ISBN / Date incompatibility (help) - ^ Wilkinson, Stephan (Jan 2003). "With the Noise of a Stone Crusher". Popular Science.
Bibliography
edit- Bingham, Victor (1998). Major Piston Aero Engines of World War II. Shrewsbury, UK: Airlife Publishing. ISBNย 1-84037-012-2.
- Christopher, John (2013). The Race for Hitler's X-Planes: Britain's 1945 Mission to Capture Secret Luftwaffe Technology. Stroud, UK: History Press. ISBNย 978-0-7524-6457-2.
- Gunston, Bill (2006). World Encyclopedia of Aero Engines: From the Pioneers to the Present Day (5thย ed.). Stroud, UK: Sutton. ISBNย 0-7509-4479-X.
- Mankau, Heinz and Peter Petrick. Messerschmitt Bf 110, Me 210, Me 410. Raumfahrt, Germany: Aviatic Verlag, 2001. ISBNย 3-925505-62-8.
- Neil Gregor Daimler-Benz in the Third Reich. Yale University Press, 1998
External links
edit- Daimler-Benz Aircraft Engines
- Aviation History.com, DB 600 series page
- Kurfรผrst - Resource on Messerschmitt Bf 109 performance.
- (1940) Betriebs und Wartungsvorschrift zum Mercedes-Benz Flugmotor DB 601 A u. B - 1940 dated operation and maintenance manual for the Daimler-Benz DB 601A and DB 601B aircraft engines[permanent dead link]
- DB 606 "power system" CAD-based animation of crankcase/conrod/piston components








